CN201132606Y - Travelling stair self-mounted on aeroplane - Google Patents

Travelling stair self-mounted on aeroplane Download PDF

Info

Publication number
CN201132606Y
CN201132606Y CNU2007200823470U CN200720082347U CN201132606Y CN 201132606 Y CN201132606 Y CN 201132606Y CN U2007200823470 U CNU2007200823470 U CN U2007200823470U CN 200720082347 U CN200720082347 U CN 200720082347U CN 201132606 Y CN201132606 Y CN 201132606Y
Authority
CN
China
Prior art keywords
escalater
sun gear
chain
autostairs
power drive
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CNU2007200823470U
Other languages
Chinese (zh)
Inventor
曹宇
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Chengdu Yuzhongmei Science and Technology Co Ltd
Original Assignee
Chengdu Yuzhongmei Science and Technology Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Chengdu Yuzhongmei Science and Technology Co Ltd filed Critical Chengdu Yuzhongmei Science and Technology Co Ltd
Priority to CNU2007200823470U priority Critical patent/CN201132606Y/en
Application granted granted Critical
Publication of CN201132606Y publication Critical patent/CN201132606Y/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Landscapes

  • Power-Operated Mechanisms For Wings (AREA)

Abstract

The utility model discloses an own autostairs on a airplane, which comprises a power drive mechanism, a vertical turbine runner shaft, a central axis, a sun gear and a chain which are arranged inside a port. The own autostairs has the advantages that the structure is simple without occupying more space; when in use, the port is let down, then the autostairs inside can connect the ground and a hatch of the airplane for lifting passengers up and down automatically; the autostairs is rapid and convenient and is suitable for all airliners.

Description

Aircraft carries escalater
Technical field
The utility model relates to a kind of escalater, especially the escalater that carries of aircraft.
Background technology
The upper and lower ladder that carries on the aircraft generally all is fixed on the hatch door.Owing to have luggage, people when upper and lower aircraft, to seem very inconvenient.Particularly those the elderlys, child or the like are all the more so.
Chinese patent CN2534098 number disclosed " the winding stair car of boarding automatically " patent (application number: 02202590.1), on motor-driven holder crossbeam, a power drive and hydraulic lift are arranged, by power takeoff and change speed gear box bonded assembly power process transmission shaft, the driving system of vertical turbine axle, center shaft, sun gear, hinge wheel and chain is rotated escalater, by hydraulic lift, can make the escalater automatic lifting again.The weak point of this patent is: this equipment can't use under emergency case, can not use at the airstrip that condition is relatively poor.
Summary of the invention
The purpose of this utility model is exactly to provide a kind of aircraft simple in structure to carry escalater, so that the passenger in time reports to the police under emergency case.
In order to achieve the above object, the aircraft that the utility model provides carries escalater and comprises power drive, vertical turbine axle, center shaft, sun gear, hinge wheel and chain, wherein, power drive, vertical turbine axle, center shaft, sun gear, hinge wheel and chain all are arranged on the hatch door inboard.Power drive, vertical turbine axle, center shaft, sun gear, hinge wheel and chain specifically be arranged as prior art, repeat no more here.When the utility model uses, put down hatch door, inboard escalater can connect ground and aircraft hatch, automatically the ascending, descending passenger.
The aircraft that the utility model provides carries escalater and has positive effect: power drive, vertical turbine axle, center shaft, sun gear, hinge wheel and chain all are arranged on the hatch door inboard, and be simple in structure, can not take more space; Put down hatch door during use, inboard escalater can connect ground and aircraft hatch, and the ascending, descending passenger is efficient and convenient automatically.
Description of drawings
The utility model will be further described in conjunction with the accompanying drawings, please referring to accompanying drawing:
Accompanying drawing 1 expression scheme drawing of the present utility model.
Structure shown in the accompanying drawing 1 comprises: aircraft 1, hatch 2, escalater 3, hatch door inboard 4, the hatch door outside 5.
The specific embodiment
The aircraft that the utility model provides carries escalater and comprises power drive, vertical turbine axle, center shaft, sun gear, hinge wheel and chain, wherein, power drive, vertical turbine axle, center shaft, sun gear, hinge wheel and chain all are arranged on hatch door inboard 4.Power drive, vertical turbine axle, center shaft, sun gear, hinge wheel and chain specifically be arranged as prior art, repeat no more here.When the utility model uses, put down hatch door, inboard escalater 3 can connect ground and aircraft 1 hatch 2, automatically the ascending, descending passenger.
The utility model protection domain relates to all changes form recited above.

Claims (1)

1, a kind of aircraft carries escalater, comprise power drive, vertical turbine axle, center shaft, sun gear, hinge wheel and chain, it is characterized in that: power drive, vertical turbine axle, center shaft, sun gear, hinge wheel and chain all are arranged on hatch door inboard 4.
CNU2007200823470U 2007-12-09 2007-12-09 Travelling stair self-mounted on aeroplane Expired - Fee Related CN201132606Y (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CNU2007200823470U CN201132606Y (en) 2007-12-09 2007-12-09 Travelling stair self-mounted on aeroplane

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CNU2007200823470U CN201132606Y (en) 2007-12-09 2007-12-09 Travelling stair self-mounted on aeroplane

Publications (1)

Publication Number Publication Date
CN201132606Y true CN201132606Y (en) 2008-10-15

Family

ID=40060880

Family Applications (1)

Application Number Title Priority Date Filing Date
CNU2007200823470U Expired - Fee Related CN201132606Y (en) 2007-12-09 2007-12-09 Travelling stair self-mounted on aeroplane

Country Status (1)

Country Link
CN (1) CN201132606Y (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104955728A (en) * 2012-11-20 2015-09-30 里尔喷射机公司 Optical viewing apparatus for aircraft doorway
CN109649632A (en) * 2018-12-07 2019-04-19 西安飞机工业(集团)有限责任公司 A kind of grounding type boarding door of aircraft

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104955728A (en) * 2012-11-20 2015-09-30 里尔喷射机公司 Optical viewing apparatus for aircraft doorway
US10252818B2 (en) 2012-11-20 2019-04-09 Learjet Inc. Optical viewing apparatus for aircraft doorway
CN109649632A (en) * 2018-12-07 2019-04-19 西安飞机工业(集团)有限责任公司 A kind of grounding type boarding door of aircraft

Similar Documents

Publication Publication Date Title
CN108146169B (en) Wing rear-folding type air-ground dual-purpose carrier
CN101998921A (en) An aircraft landing gear arrangement and a nose landing gear assembly
CN204915162U (en) Navy, army and air force four -axis binary vehicle
CN108859640B (en) Air-ground dual-purpose aircraft
CN102285449A (en) Coaxial double-rotor wing ducted aircraft
CN103935517B (en) Aircraft
CN105329056A (en) Wheel type rotor wing vehicle
CN201132606Y (en) Travelling stair self-mounted on aeroplane
CN103072689B (en) Slow speed of revolution double-layer propeller helicopter
CN205554569U (en) Aerospace's undercarriage is exclusively used in
CN106114842A (en) A kind of oil electricity mixing coaxial dual-rotor helicopter and using method thereof
CN202429351U (en) Auxiliary device for takeoff powered parawing
CN201553300U (en) Electric paramotor
CN205524948U (en) Unmanned autogyro
CN107600395A (en) A kind of power wheel electric driver of civil aircraft undercarriage
CN204737021U (en) Solar energy dirigible of double dynamical dual fail -safe
CN109131846B (en) Manual steering device of undercarriage
CN204895860U (en) Uniclinal changes rotor fuselage and holds up vertical take -off and landing aircraft
RU2485016C1 (en) Bogdanov's device for carrier lifting and transfer
CN207328816U (en) A kind of power wheel electric driver of civil aircraft undercarriage
CN100441258C (en) Power assembly of model airplane
CN104890850A (en) Dual-power dual-insurance solar airship
CN203461094U (en) Simple solar flight vehicle
CN106671712B (en) Flying electric vehicle
CN204956924U (en) Aircraft

Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
C17 Cessation of patent right
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20081015

Termination date: 20100111